Patent application number | Description | Published |
20080210490 | Ladder System, Especially For Vehicles - The invention relates to a ladder comprising a single post ( | 09-04-2008 |
20080210813 | FRONT AIRCRAFT PART COMPRISING A FLAT PARTITION BETWEEN A PRESSURISED ZONE AND A NON-PRESSURISED ZONE HOUSING LANDING GEAR - The present invention relates to a front aircraft part ( | 09-04-2008 |
20080223984 | Aircraft comprising a landing gear compartment permitting better integration of the landing gear - The object of the invention is an aircraft comprising at least one gear compartment in which is adapted to be disposed a landing gear ( | 09-18-2008 |
20080290769 | Electrical Cabinet with Electrical Connection to Its Door - The invention concerns an electrical cabinet ( | 11-27-2008 |
20090050739 | COCKPIT AND AIRCRAFT INCLUDING SUCH COCKPIT - A cockpit and an aircraft including such cockpit. The cockpit includes a front section of an aircraft. Such cockpit includes a pressure bulkhead sealing the section and a pressurization system for pressurizing such section. | 02-26-2009 |
20090078819 | Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft - The disclosed embodiments relates to a jet engine for an aircraft, characterized in that it bears at least one stabilizer, the stabilizer being fastened on the rigid structure of said jet engine so as to form a one-piece assembly. The jet engine can also bear one or more auxiliary devices required for the operation of the jet engine. The disclosed embodiments also relates to an aircraft provided with such a jet engine, and to a method of mounting such a jet engine on an aircraft. | 03-26-2009 |
20090159743 | CASING AND FRONT LANDING GEAR ASSEMBLY FOR AN AIRCRAFT - The casing comprises a wall defining an internal housing open on the bottom in order to allow the retraction of a corresponding front landing gear into the interior of the housing. The said wall separates the said non-pressurized internal housing from a surrounding pressurized zone of the aircraft. A reinforcement structure is provided around the wall on the side of the surrounding pressurized zone. The separation wall is a shell coming to envelop the shape of the front landing gear, on the side opposite the opening of the internal housing, and the reinforcement structure comprises on the one hand longitudinal reinforcement elements extending on both sides of the shell and on the other hand transverse reinforcement elements connecting the longitudinal reinforcement elements. The shell has a first zone of considerable width accommodating the wheels of the landing gear, a second zone of lesser width accommodating the rod of the landing gear, and a third zone running from the second zone of lesser width, becoming wider and accommodating a portion of the mechanism for deployment/retraction of the landing gear. As a variant or in combination, the shell has on the one hand a front area of considerable height accommodating the wheels of the landing gear and on the other hand a rear area of lesser height accommodating the rod and a portion of the mechanism for deployment/retraction of the said landing gear and above which there extends at least one transverse reinforcement element making it possible to provide support for an equipment item of the aircraft. | 06-25-2009 |
20090308973 | AIRCRAFT TAIL CONE - In a rear cone of a fuselage of an airplane a pressurized space is arranged in the rear cone and extends up to an impervious strong wall, placed on a rear portion of the length covered by a fin. The pressurized space constitutes an area accessible to individuals and is able to constitute, in particular, a rest and service area for the crew. | 12-17-2009 |
20100001129 | STORAGE COMPARTMENT FOR THE NOSE GEAR OF AN AIRCRAFT - A front landing gear storage compartment configured for an airplane including a set of retractable landing gears including a front gear centered on a longitudinal median plane of the fuselage. The storage compartment forms an impervious partition between a pressurized zone and the housing for the front gear in its retracted position, and includes a reinforced upper face including a more or less flat zone, more or less horizontal when the airplane is on the ground, so as to form a floor of a pressurized area of the airplane. | 01-07-2010 |
20100140396 | AIRCRAFT HOLD AND AIRCRAFT EQUIPPED WITH SUCH A HOLD - A device for keeping objects, especially luggage, in an aircraft hold, the device including a flexible partition and at least one winding mechanism. The flexible partition is mounted on the winding mechanism such that it can be both wound onto the winding mechanism or unwound from the winding mechanism. The flexible partition includes an attaching mechanism that operates with a complementary mechanism to maintain the flexible partition in an unwound position. | 06-10-2010 |
20100170992 | CONVEYOR DEVICE INTENDED IN PARTICULAR FOR LUGGAGE IN AN AIRCRAFT HOLD - A device intended for a hold that can receive containers and luggage simultaneously. The hold includes a freight loading system including rollers defining a rolling surface on which a container can move with the movement of the rollers. The device includes a unit including conveyor belts disposed longitudinally in the hold one after the other such as to extend over at least part of the length of the hold. Each conveyor belt includes an upper section configured to receive an object to be moved and each conveyor belt can move between a first raised position in which the upper section of the belt is located above the rolling surface defined by the rollers of the freight loading system and a second position in which the upper section of the belt is located below the rolling surface. | 07-08-2010 |
20100176240 | LANDING GEAR CASING WITH REDUCED SPACE REQUIREMENT - The invention relates to a landing gear casing that comprises a longitudinal box with walls defining an inner housing ( | 07-15-2010 |
20100176241 | AIRCRAFT FRONT PORTION INCLUDING A CONCAVE BULKHEAD SEPARATING A NON-PRESSURIZED RADOME AREA AND A PRESSURIZED AREA - The invention relates to an aircraft front portion ( | 07-15-2010 |
20100181425 | ITEM OF AIRCRAFT GALLEY FURNITURE AND AIRCRAFT COMPRISING SUCH AN ITEM OF FURNITURE - The invention relates to an item of aircraft galley furniture separating a cockpit ( | 07-22-2010 |
20100181429 | DEVICE FOR MOVING OBJECTS, INTENDED IN PARTICULAR FOR LUGGAGE IN A HOLD OF AN AIRCRAFT - The invention relates to a device for moving objects, particularly luggage, in an aircraft hold, said device including a moving wall ( | 07-22-2010 |
20100187355 | HOLD LAYOUT DEVICE FOR AN AIRCRAFT FOR CREW-MEMBER REST AND AIRCRAFT COMPRISING SAME - The invention relates to a device for developing an aircraft hold located under the floor of the passenger cabin and the cockpit and including a so-called commercial area in which freight can be transported and a technical area including technical equipment and located at the front of the commercial area an at least partially under the cockpit, wherein said device includes: at least one compartment sealed relative to the hold located at the front of said commercial area and at the back of a portion at least of the technical area; a staircase connecting each compartment to a portion of the intermediate floor between the passenger cabin and the cockpit; and a sealed corridor extending from said staircase to each of said sealed compartments. | 07-29-2010 |
20100187356 | AIRCRAFT COMPRISING A PLATFORM THAT CAN BE MOVED BETWEEN TWO LEVELS OF THE AIRCRAFT - An aircraft with at least two levels situated one above the other, including: a platform that can be moved between a first position and a second position, the first of these positions, as a lower position, being situated at a first level of the aircraft and the second position, as a higher position, being situated at a second level higher than that of the first level; an assembly of traction cables connected on the platform and a mechanism operating the cables for raising and lowering the platform; and an assembly of walls surrounding at least partially the platform and along which the platform moves. | 07-29-2010 |
20100219291 | AIRCRAFT HOLD INTENDED TO ACCOMMODATE BAGGAGE - An aircraft hold including a floor having a substantially flat central part and a side part disposed along each longitudinal edge of the central part and inclined in relation thereto. The aircraft hold also includes at least one bench with a seat that can move between a position in which it is substantially parallel to the central part of the floor and a position in which it is folded against a wall of the hold. | 09-02-2010 |
20100301163 | STAIRWAY FOR AN AIRCRAFT - A stairway used for gaining access from a theoretically horizontal lower level to a theoretically horizontal higher level, and including a succession of intermediate steps between these two levels. A subassembly of intermediate steps corresponding to the steps closest to the lower level is mobile between a first deployed position at which the lower intermediate steps are in the extension of other intermediate steps, and a raised position at which the lower intermediate steps are in a substantially vertical position. | 12-02-2010 |
20110192933 | MAST FOR SECURING AN ENGINE TO AN AIRCRAFT WING - A securing mast for securing an engine to the wing of an aircraft, wherein the device includes two fasteners, a first eng of each fastener being secured to the engine and the second end of each fastener being secured to the wing, wherein the fasteners include hinged junction means capable of modifying the geometry of the aforementioned fasteners in order to modify a distance between the engine and the wing. | 08-11-2011 |
20110260003 | AIRCRAFT SEAT ASSEMBLY STRUCTURE, AND FITTED FUSELAGE - An aircraft seat assembly structure ( | 10-27-2011 |
20120193472 | STAIRWAY FOR AN AIRCRAFT - A stairway used for gaining access from a theoretically horizontal lower level to a theoretically horizontal higher level, and including a succession of intermediate steps between these two levels. A subassembly of intermediate steps corresponding to the steps closest to the lower level is mobile between a first deployed position at which the lower intermediate steps are in the extension of other intermediate steps, and a raised position at which the lower intermediate steps are in a substantially vertical position. | 08-02-2012 |
20120268866 | Method Of Equipments Integration For A Complex Electrical Heart And Module Of Implementation - The invention aims at simplifying the electrical connections between equipment and an electrical power centre to be supplied in electricity, while enabling a good accessibility of each piece of equipment and an easier maintenance. To do so, a particular integration of this equipment is carried out so as to be able to assemble them together and connect them in a direct extension of the electrical power centre. According to one embodiment, an integration module consists in a frame and a cover, the frame having a substantially parallelepipedic shape adapted to be able to extend longitudinally along a main axis in parallel with a longitudinal main side of the electrical power centre of the structure to be supplied. Cells of constant section and a width being adjustable by movable intermediary walls, extend perpendicularly to the main axis. Such cells are adapted to receive formatted electrical equipment. | 10-25-2012 |
20120285950 | ELECTRICAL POWER DISTRIBUTION UNIT AND A VEHICLE HAVING SUCH A UNIT - In an electrical cabinet ( | 11-15-2012 |
20120292960 | HEADREST FOR A PASSENGER SEAT FOR AN AIRCRAFT - The aircraft passenger seat headrest ( | 11-22-2012 |
20130082138 | VENTILATION SYSTEM, AIR BLOWING AND EXTRACTION CIRCUITS OF SUCH A SYSTEM, AS WELL AS AN AIRCRAFT AVIONICS BAY - A ventilation system for an avionics bay has two strut assemblies for stiffening the floor of the cockpit, each strut assembly being arranged symmetrically regarding to the central plane of the aircraft, and means of distribution of the blowing air in the cabinets of the bay from the strut assemblies. The extraction circuit includes exhaust ducts integrated in the cabinets and couples together by tight inter-cabinets junctions in an overall configuration of maximized compactness. | 04-04-2013 |
20130084792 | METHOD OF INTEGRATING AN AVIONICS BAY AND FLOOR STRUCTURE FOR IMPLEMENTATION - An integrated avionics bay in a floor area can be provided with adequate ventilation. The structure of an aircraft cockpit floor is able to integrate at least one bay, with a walking floor in the cockpit, a structural volume and a bay integrated in a space of the liberated structural volume. The bay as integrated in a horizontal position in this space includes a peripheral frame with at least one protective cover with a direct access to the bay at the floor level and a lower wall with a rear face access. Side openings formed in the frame can couple with vertical walls to allow fresh air blowing from the rear wall of the bay via a flow from rearwards to upwards to reach the top cover and an air extraction by an upper surface extractor. | 04-04-2013 |
20130112808 | COMPACT IMPROVED AIRCRAFT LANDING GEAR - A breaker strut of an aircraft landing gear, including means to adjust the length of at least one of its lower and upper portions and/or a space allowing a nesting of the lower and upper portions in the folded position of the strut. A landing gear including such a strut and/or retraction means including two slider-crank mechanisms which are phase shifted by a non-zero angle φ allowing a reduction of the variations of torque C applied to the undercarriage of the gear as it moves between the lowered and raised states of the latter. | 05-09-2013 |
20130126671 | Unknown - There is provided an aircraft folding seat ( | 05-23-2013 |
20130148325 | BRACKET FOR DISPLAY DEVICES FOR AN AIRCRAFT COCKPIT - The support such as an instrument panel or a glare shield, for supporting display devices in an aircraft cockpit, comprises a glare shield comprising a core of cellular structure and two skins covering opposite faces of the core. | 06-13-2013 |
20130160768 | OXYGEN SUPPLY SYSTEM INTENDED IN PARTICULAR FOR THE FLIGHT CREW OF AN AIRCRAFT - This system is intended for supplying oxygen in particular for the flight crew of an aircraft. It comprises an oxygen source, an oxygen mask as well as a circuit connecting the oxygen source to the said oxygen mask. | 06-27-2013 |
20130221156 | AIRCRAFT NOSE STRUCTURE AND CORRESPONDING AIRCRAFT - This aircraft nose structure comprises frames ( | 08-29-2013 |
20130228655 | METHOD AND DEVICE FOR FITTING OUT AN AIRCRAFT NOSE COMPARTMENT IN AN AVIONICS BAY - An aerodynamic body, with at least one ancillary flap arranged such that it can be moved on the aerodynamic body with the aid of a guide mechanism, and with a drive device for purposes of actuating the ancillary flap, the guide mechanism having a pivotal articulation, by which the ancillary flap is articulated on the aerodynamic body such that it can be extended, and which is arranged in a rear region of the ancillary flap as viewed in the flow direction. | 09-05-2013 |
20130259612 | AUTOMATED STORAGE CABINET FOR TROLLEYS, AND AIRCRAFT INCORPORATING SUCH A CABINET - The present invention relates to an automated storage cabinet for trolleys. It includes a device for automatically handling a single trolley with a handling basket including a vertical plate perpendicular to the waiting area, vertically movable between the floor of the waiting area and any one of the levels of the trolley storage cabinet, and two side flanks, connected to the vertical plate and provided with structure for supporting, on either side, two opposite sides of a trolley in the waiting area and for transferring the supported trolley through an opening of the predetermined compartment. The handling device can include structure for inserting the trolley into or extracting the trolley from the predetermined compartment. | 10-03-2013 |
20130292513 | SECURED VESTIBULE TO THE COCKPIT OF AN AIRCRAFT AND AIRCRAFT EQUIPPED WITH SUCH AN ACCESS DOOR - The invention relates to a secure access airlock enabling the communication between several rooms of an aircraft, the secure airlock being installed in an area of the aircraft between a first room and at least one second room, characterized in that it includes two mobile partitions provided in the form of portions of concentric cylinders, each of the partitions being capable of being moved, separately from one another, about a common axis, so as to provide a single opening therebetween which makes it possible to access either of the rooms, the two partitions being capable of moving over two concentric cylinders having different diameters. | 11-07-2013 |
20130333857 | HEAT EXCHANGER INCORPORATED INTO A WALL OF AN AIRCRAFT - An aircraft includes at least one wall delimiting a first zone (I) of the aircraft which is thermally insulated from the outside of the aircraft and a second zone (E) contained within the aircraft which is not thermally insulated with respect to the outside of the aircraft and a heat exchanger inside which a heat transfer fluid circulates, wherein the wall includes at least one duct inside which the heat transfer fluid circulates so as to act as a heat exchanger. | 12-19-2013 |
20140042272 | CENTRE PEDESTAL FOR AIRCRAFT COCKPIT AND AIRCRAFT COMPRISING SUCH A PEDESTAL - The invention relates to an aircraft cockpit centre pedestal for the attachment of control and instrumentation equipment for this aircraft, wherein the centre pedestal includes an equipment module including controls connected to at least one first electrical connector, and a single-piece frame including an upper face provided with a recess including at least one second electrical connector installed at the bottom of the recess and connected to computers onboard this aircraft in which this equipment module is installed, the at least one first electrical connector of the equipment module being inserted into at least one second electrical connector so as to connect the controls of the equipment module and these onboard computers. The invention also relates to an aircraft including such a pedestal. | 02-13-2014 |
20140110529 | AIRCRAFT FUSELAGE AND METHOD FOR CONSTRUCTING A FLOOR IN SUCH A FUSELAGE - Such a fuselage includes cross-members adapted for the formation of a floor, at least one of said cross-members including an upper part, a lower part, linkage for the lower part to the upper part, and at least one opening for the passage of systems which is delimited between the lower part and the upper part. The upper part of the cross-member is fastened to the fuselage and is dimensioned so as to bear the stresses to which said cross-member may be subjected when the aircraft remains on the ground. The lower part is fastened to the upper part so as to reinforce it such that when assembled, the upper part and the lower part are adapted to bear the stresses to which the cross-member may be subjected in flight conditions of the aircraft. | 04-24-2014 |
20140145128 | Method for installing a wiring harness in an aircraft and tool for implementing said method - A method for installing a wiring harness in an aircraft. The method comprises using cables having first ends secured to the harness and winding means onto each of which is wound one of said cables so as to lift up said harness by exerting a tensile force. The first ends of the cables are distributed along at least a section of the harness so as to distribute the tensile forces over the section. | 05-29-2014 |
20140159444 | SEATING DEVICE COMPRISING A FORWARD-FOLDABLE BACKREST - A seating device with reduced bulk, for example for an aircraft. This seating device comprises a backrest which describes a circular translational movement towards the front and upwards of the device when the seating device is brought to the retracted configuration. A seating structure is provided comprising a bearing piece on which are fixed, side by side, a plurality of seating devices with reduced bulk. An aircraft is provided comprising a seating device with reduced bulk mounted in its cabin. | 06-12-2014 |
20140159450 | AIRCRAFT SEAT BACK WITH IMPROVED COMFORT AND REDUCED SIZE - The invention relates to a seat back for an aircraft comprising a structural column bearing a plurality of devices for supporting an occupant of the seat, these devices being distributed along the structural column and oriented transversely relatively to the structural column so as to each protrude on either side of this column. This solution can reduce the mass and dimensions, while providing satisfactory comfort for the occupant. | 06-12-2014 |
20140165285 | TOILET AREA FOR AN AIRCRAFT CABIN, IN PARTICULAR FOR A FLYING WING AIRCRAFT - A toilet area for an aircraft cabin comprising an access door and housing a toilet bowl. The toilet area also comprises an evacuation exit, the access door occupying a closed position in the toilet area in a toilet configuration and a folded position in the toilet area in an evacuation configuration. Usage in particular in a flying wing aircraft is provided. | 06-19-2014 |
20140166806 | PIECE OF FURNITURE FOR AN AIRCRAFT INCLUDING MEANS FOR DISTRIBUTING A CARRIAGE BETWEEN TWO SECTIONS - A piece of furniture for an aircraft, including a plurality of carriages a first section forming an interface of use for a user with which at least one carriage may be taken and/or deposited in the piece of furniture and a second section allowing the said carriages to be circulated along at least first and second main directions substantially perpendicular to each other, at least in a plane of the aircraft for storing and/or delivering to the user at least one carriage, the first section and/or the second section including an arrangement for distributing at least one carriage from the second section towards the first section and vice versa. | 06-19-2014 |
20140168907 | OVERHEAD PANEL FOR AN AIRCRAFT COCKPIT AND AIRCRAFT INCLUDING SUCH A PANEL - The invention relates to an overhead panel able to be positioned in an aircraft cockpit, which includes an assembly of independent submodules ( | 06-19-2014 |
20140175220 | AIRCRAFT COCKPIT WITH EMERGENCY EXIT VIA A CENTRAL PANE - The present invention relates to an aircraft cockpit with a double flight deck in which a central pane of a windscreen can be removed in order to at least partially clear an opening in order to constitute an emergency exit and ensure natural ventilation of the cockpit. Moreover, a central portion of a glare shield and of a flight station instrument panel are optionally moveable in order to facilitate access to the opening in the event of the need for emergency evacuation. | 06-26-2014 |
20140175223 | AIRCRAFT FRONT PORTION HAVING AN IMPROVED LANDING GEAR BAY - An aircraft front portion in which the landing gear storage bay is arranged under a cockpit floor. The landing gear bay is mechanically connected to the fuselage frames of the aircraft front portion in order to perform the function of taking up the mechanical forces acting on the fuselage frames under the effect of pressurization. The cockpit floor is thus simplified since it serves solely as a plane for the crew to walk on and it can be lowered so as to release space in the cockpit. | 06-26-2014 |
20140175224 | AIRCRAFT NOSE WITH COCKPIT AND AVIONICS BAY MODULES INTEGRATED THEREIN - An aircraft nose comprising a primary fuselage structure, and housed inside said structure, a cockpit, and an avionics bay containing a plurality of avionics racks designed to receive electrical and/or electronic equipment. The cockpit and the avionics bay are each made in the form of a distinct module that is suitable for being installed in a single operation inside the primary fuselage structure. The use of modules for integrating in the aircraft nose makes it possible to reduce considerably the time required for fitting out the nose on the final assembly line of the aircraft. | 06-26-2014 |
20140175225 | AIRCRAFT COCKPIT HAVING A LOWERED FLOOR FOR WALKING ON - A cockpit for an aircraft nose, the cockpit having a floor that acts solely as a floor for the crew to walk on and that is lower than the height of the cabin floor situated behind the cockpit. The cockpit also has a stair connected to the floor in order to enter and leave the cockpit. This arrangement enlarges the volume of the cockpit and enables equipment to be housed therein that previously used to be housed in the zone that is difficult to access that is situated under the cockpit and that also contains the bay for storing landing gear. | 06-26-2014 |
20140175226 | Avionics cargo hold module having an upper integrated floor - An integral avionics bay module. The module has a structure that has an integral cabin floor on top that closes the structure. Installing such an integral avionics bay structure in a single operation inside a primary fuselage structure considerably reduces the integration time on the final assembly line for the aircraft. | 06-26-2014 |
20140175228 | METHOD FOR AUTOMATED AND INDIVIDUALIZED PROCESSING OF LUGGAGE IN AN AIRCRAFT AND AIRCRAFT HOLD FOR IMPLEMENTING SAME - An aircraft hold including a device for automated processing of luggage is provided. The device includes at least one automated arm for handling the luggage. The automated arm, which is mounted so as to be able to move in translation along the longitudinal axis of the hold of the aircraft includes a head for grasping an item of luggage. A wrapper for packaging an item of luggage for the automated processing of the item of luggage is also provided. The wrapper is in the form of a protective film and includes a grasping surface separate from but secured to the protective film. A method for automated processing of luggage in an aircraft is provided. | 06-26-2014 |
20140175229 | METHOD FOR AUTOMATED AND ORDERLY PROCESSING OF LUGGAGE IN AN AIRCRAFT - A method for automated processing of luggage in an aircraft is provided. The hold of the aircraft includes a device for automated processing of the luggage. The method includes the device for automated processing operating in an autonomous manner to load the luggage into the hold of the aircraft, with each item of luggage being packaged to this end in a packaging wrapper comprising visual markers. The method includes the device for automated processing viewing these visual markers. | 06-26-2014 |
20140175964 | ELECTRICAL AND ELECTRONICS BAY OF AN AIRCRAFT WITH AN IMPROVED ARCHITECTURE AND AIRCRAFT INCORPORATING SAID BAY - An electrical and electronics bay of an aircraft comprising two rows of elements, each row being separated by a single corridor and comprising at least one set of systems elements and at least one electrical power center, the systems elements being arranged in cabinets. At least one of the cabinets comprises mobile shelves for allowing access to the back of the cabinets by crossing it. This architecture makes it possible to increase the density of the elements present in the bay while observing the principles of redundancy and segregation. | 06-26-2014 |
20140179211 | AIR EXTRACTION UNIT FOR AVIONICS BAY - An air extraction unit taking the form of a body, the geometric shape of which makes it easier to incorporate into an avionics bay of an aircraft. The air extraction unit derives from a multipurpose approach to the operational components of the avionics bay of an aircraft aimed at achieving weight and cost savings. All of the elements of the air extraction circuit are arranged in a compact housing of the body and are protected by the structure thereof. The air extraction unit can be used as a floor of an avionics bay that can be walked on, with a lateral organization. | 06-26-2014 |
20140209740 | AIRCRAFT COCKPIT, IN PARTICULAR THE FRONT PORTION OF AN AIRCRAFT COCKPIT - A device for mixing at least two separate streams of components which, when mixed, form a combined fluid stream. The device comprises a conduit with at least two separate passageways leading to exit openings at an end face of the conduit. Each passageway communicates with a separate component stream and is arranged to direct the separate component stream in a downstream direction. The exit openings each have a predetermined cross-sectional flow area. A separate channel is located at a downstream end of each passageway exit opening. The channels are arranged to redirect the flow from each passageway to an axial direction. A single mixing chamber communicates with all of the separate channels, the mixing chamber being arranged to receive each of the component streams at an upstream end thereof and to permit a mixing of the component streams. An outlet is arranged downstream of the mixing chamber through which the combined fluid stream is dispensed. | 07-31-2014 |
20140209742 | AIRCRAFT ELECTRICAL CORE - An electrical core of an aircraft is provided. The electrical core includes at least one shelf on which is disposed at least one module containing components and comprising at least one input able to be linked to at least one power supply cable and at least one output able to be linked to at least one output cable. In the module, the output cable or cables travel under or in the shelf disposed under the module. | 07-31-2014 |
20140210258 | ELECTRICAL CABINET OF AN AIRCRAFT INCORPORATING AN IMPROVED ELECTRICAL CONNECTION SYSTEM - An electrical cabinet of an aircraft is provided. The electrical cabinet includes at least one motherboard including on a first face sockets into which are plugged PCB boards ensuring one or more electrical functions, the said electrical cabinet being linked to the electrical circuit of the aircraft organized as various electrical harnesses by way of an electrical connection system, characterized in that the electrical connection system comprises at the level of the second face of the motherboard at least one additional layer, the free face of the last additional layer comprising sockets each ensuring electrical connection with an electrical harness of the aircraft, the additional layer or layers comprising tracks which make it possible to reorganize the electrical circuits emanating from the sockets intended for the PCB boards so as to render them compliant with the sockets intended for the harnesses of the aircraft. | 07-31-2014 |
20140246542 | Front landing-gear well - A forward part of an aircraft comprising a fuselage and a landing gear well housing a forward landing gear comprising a breaker strut designed to adopt an extended configuration when the landing gear is extended, configuration in which said breaker strut lies in a strut plane parallel to the transverse direction of the forward part. The forward part comprises a transverse beam resisting strut reactions located above the landing gear well and mounted on the fuselage at its two ends, the beam having a globally rectangular cross-section, in which the median plane parallel to the length of the rectangle is coincident with said strut plane. | 09-04-2014 |
20140301023 | ASSEMBLY OF COMPACTLY INTEGRATED CONTACTORS IN AN ELECTRICAL CORE - An electrical core comprising an assembly of power management and distribution contactors is provided. The power management contactors are attached to a first support element and the distribution contactors are carried by a second support element superimposed on the first so as to form a multilayer assembly. The distribution contactors are arranged in double symmetry about two axes perpendicular to one another. They are mechanically linked through a mechanical linkage element extending between two rows of contactors and which carries electrical connection elements connecting the contactors to an element for connecting to a power source. The contactors are assembled in modules according to their type. In particular, the management module comprises at least one modular element common to the power management contactors which is suitable for performing a given secondary function other than the function of establishing a contact. | 10-09-2014 |
20150024638 | Power breaker strip for the fixed-pitch connection of several electrical cables lines - A power breaker strip comprising a strip support and a plurality of interphase spacer elements, and a plurality of interline spacer elements, assembled with the plurality of interphase spacer elements such that each interline spacer element extends at least partly between two consecutive interphase spacer elements. The interphase spacer elements and the interline spacer elements together delimit a plurality of per pitch zones of the strip in which connection terminals of several lines of electrical cables can be inserted. | 01-22-2015 |
20150084491 | Electronics Cabinet With Ventilation System - A cabinet designed to accommodate at least one item of electronic equipment and a system for interconnecting such a cabinet with the external networks for blowing and extracting air. The system includes at least one of a blowing inlet and an extracting outlet including a plurality of orifices and at least one hollow structural upright as a part of the blowing circuit or of the extracting circuit. | 03-26-2015 |